Q1/Calculate the power in kilowatts of the gas turbine power plant has a greatesttemperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of theturbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of theair that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process takeC,= 1.11 kJ/kg:K, y=1.333, and at the compression process take c,= 1.005kJ/kg K, and y =1.42045.74 kW2085.71 kW1025.73 kW1095.72 kWQ2/ Calculate the thermal efficiency of the heat engine working on the diesel cycletakes in air at 1 bar, 20 °C, and a compression ratio 12 and the highest temperatureduring the cycle was 1100 °C. Take c,= 1.005 kJ/kg-K, c,= 0.718 kJkg-K forair.63 %53 %58 %68 %

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Q1/Calculate the power in kilowatts of the gas turbine power plant has a greatest temperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of the turbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of the air that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process take Cp= 1.11 kJ/kg•K, y=1.333, and at the compression process take c,= 1.005 kJ/kg-K, and y =1.4 2045.74 kW O 2085.71 kW 1025.73 kW 1095.72 kW O

Q1/Calculate the power in kilowatts of the gas turbine power plant has a greatest temperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of the turbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of the air that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process take Cp= 1.11 kJ/kg•K, y=1.333, and at the compression process take c,= 1.005 kJ/kg-K, and y =1.4 2045.74 kW O 2085.71 kW 1025.73 kW 1095.72 kW O

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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QI/Calculate the power in kilowatts of the gas turbine power plant has a greatest temperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of the turbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of the air that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process take Cp= 1.11 kJ/kg:K, y=1.333, and at the compression process take c,= 1.005 kJ/kg K, and y =1.4
Q1/Calculate the power in kilowatts of the gas turbine power plant has a greatest temperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of the turbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of the air that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process take C,= 1.11 kJ/kg-K, y=1.333, and at the compression process take c,= 1.005 kJ/kg K, and y =1.4 1025.73 kW O 1095.72 kW 2085.71 kW O 2045.74 kW
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Q1/Calculate the power in kilowatts of the gas turbine power plant has a greatest temperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of the turbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of the air that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process take Cp= 1.11 kJ/kg:K, y =1.333, and at the compression process take c,= 1.005 kJ/kg·K, and y =1.4
Q1/Calculate the power in kilowatts of the gas turbine power plant has a greatest temperature of 700°C and a pressure ratio of 10. The isentropic efficiencies of the turbine and compressor are 0.85 and 0.82 respectively. The mass flow rate of the air that inlet to the compressor is 15 kg/s at 15 °C. At the expansion process take Cp= 1.11 kJ/kg:K, y =1.333, and at the compression process take c,= 1.005 kJ/kg K, and y =1.4 2085.71 kW O 2045.74 kW 1025.73 kW 1095.72 kW
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